N676AN
Operators of this aircraft
Who operated this tail, and how firmly we know it.
| Operator | Role | Period | Basis |
|---|---|---|---|
| AMERICAN AIRLINES, INC. (AALA) | Operator | on 2013-09-19 | Operator named in NTSB report |
Accident & incident history
Operated by AMERICAN AIRLINES INC (per NTSB report)
Maintenance disclosures
Service Difficulty Reports filed with the FAA for this airframe. Filing is largely voluntary — the number of reports is not a measure of reliability. To verify a report, search its control number at the FAA SDRS site.
104 reports on file, 1999-07-26 – 2018-09-28.
Part: SKIN — NONE (ZONE 100) · airframe 55,540 hrs · 19,631 cycles
PER NR 254 AND GA-EO-18-001 AFTER REMOVAL OF ANTENNA DOUBLER FOR AIRCELL SYSTEM AT STA 510 BTWN STR27-28R, REPAIR FUSELAGE AS REQ.
Part: WEDGE — DENTED (NR 4 SLAT) · airframe 55,540 hrs · 19,631 cycles
#4 SLAT UPPER SURFACE T/E WEDGE HAS AN OUT OF LIMIT DENT AT 19" FROM I/B END.
Part: ELEVATOR — NONE (LEFT) · airframe 55,540 hrs · 19,631 cycles
PREVIOUS REPAIR FOUND ON LH ELEVATOR LOWER SURFACE, APPROX. 84" FROM OB END. INSPECT AND REPLACE IF FOUND TO BE A TEMPORARY REPAIR. ANNOTATE STATION LOCATIONS AND FINAL DIMENSIONS OF NEW REPAIR.
Part: SKIN — NONE (ZONE 100) · airframe 55,540 hrs · 19,631 cycles
PER NR254 AND GA-EO-18-001, AFTER REMOVAL OF ANTENNA DOUBLER FOR AIRCELL SYSTEM AT STA 1350 BTWN STR29R-30, REPAIR FUSELAGE AS REQ.
Part: SKIN — DENTED (NR 2 SLAT) · airframe 55,540 hrs · 19,631 cycles
MULTIPLE DENTS FOUND ON #2 SLAT UPPER SURFACE OF AFT WEDGE.
Part: SKIN — DENTED (BS 1389) · airframe 55,540 hrs · 19,631 cycles
A DENT WAS FOUND ON AIRCRAFT SKIN, BS 1389, STRINGERS 25L & 26L.
Part: SKIN — GOUGED (ZONE 200) · airframe 55,540 hrs · 19,631 cycles
GOUGE ON INTERNAL DOUBLER AT B.S. 298, UNDER STR .20R
Part: SKIN — DENTED (HORIZONTAL STAB) · airframe 55,540 hrs · 19,631 cycles
DENT AND GOUGE FOUND ON THE LOWER SURFACE OF THE RT HORIZONTAL STABILIZER APPROXIMATELY 14 INCHES AFT OF AUX SPAR, 112 INCHES FROM INBD END.
Part: SKIN — DAMAGED (BS 1430) · airframe 55,540 hrs · 19,631 cycles
AFTER REMOVAL OF ANTENNA DOUBLER AT BS 1430 BETWEEN STRINGERS 1L AND 2L, REPAIR THE SKIN.
Part: SKIN — DENTED (BS 1787-1862) · airframe 55,540 hrs · 19,631 cycles
MULTIPLE DENTS FOUND ON THE SKIN PANEL BETWEEN STRINGERS 3L & 5L, BS 1787-1862.
Part: SKIN — CORRODED (LT WING TE FLAP) · airframe 55,540 hrs · 19,631 cycles
LEFT OTBD FLAP UPPER AREA INSIDE FLAP WAS CORRODED.
Part: SKIN — DENTED (LT WING SLAT) · airframe 55,540 hrs · 19,631 cycles
NR 1 SLAT LOWER INTERIOR WEDGE AREA HAS AN OUT OF LIMIT DENT LOCATED 43 INCHES FROM THE OTBD END AND 4.5 INCHES FROM THE T/E.
Part: SKIN — DENTED (LT WING SLAT) · airframe 55,540 hrs · 19,631 cycles
NR 1 SLAT UPPER SURFACE WEDGE HAS AN OUT OF LIMITS DENT, LOCATED 14.5 INCHES FROM THE OTBD END AND 2 INCHES FROM T/E.
Part: FILL PORT — CORRODED (LT WING) · airframe 55,540 hrs · 19,631 cycles
LEFT WING FUEL FILL PORT LANDING CORRODED.
Part: SKIN — DENTED (BS 1677) · airframe 55,540 hrs · 19,631 cycles
DENT FOUND ON FUSELAGE SKIN AT BS 1677, STRINGERS 25L TO 26L.
Part: SKIN — DENTED (VERTICAL STAB) · airframe 55,540 hrs · 19,631 cycles
VERTICAL STABILZER RT SIDE SKIN WAS DENTED APPROXIMATELY 5 INCHES FROM L/E OF AUX SPAR AND VSS 230.
Part: FRAME — GOUGED (BS 1640) · airframe 55,540 hrs · 19,631 cycles
MAIN CABIN, RT SIDE BS 1640 FRAME WAS GOUGED AT STRINGER 6R.
Part: SKIN — DENTED (RT WING SLAT) · airframe 55,540 hrs · 19,631 cycles
NR 9 SLAT UPPER SURFACE AFT WEDGE HAD A DENT THAT WAS OUT OF LIMITS, 5.75 INCHES FROM INDB END, AND .075 INCH FROM AFT EDGE.
Part: SKIN — DENTED (LT WING LE SLAT) · airframe 55,540 hrs · 19,631 cycles
LT WING NR 1 SLAT INTERIOR WEDGE WAS DENTED ON THE LOWER SURFACE, 22 INCHES FROM THE OTBD END, AND 4 INCHES FROM T/E.
Part: SKIN — DENTED (LT WING SLAT) · airframe 55,540 hrs · 19,631 cycles
NR 1 SLAT INTERIOR WEDGE HAS A DENT THAT WAS OUT OF LIMITS. 53 INCHES FROM THE OTBD END AND 5.3 INCHES FROM THE T/E.
Part: SKIN — DENTED (LT WING SLAT) · airframe 55,540 hrs · 19,631 cycles
NR 2 SLAT UPPER SURFACE T/E WEDGE HAD TWO DENTS OVERLAPPING AT 73 INCHES FROM INBD END AND 6 INCHES FROM T/E, FOUND TO BE OUT OF LIMITS.
Part: SKIN — DENTED (LT WING SLAT) · airframe 55,540 hrs · 19,631 cycles
NR 5 SLAT UPPER SURFACE, AFT WEDGE HAD A DENT THAT WAS OUT OF LIMITS. 8 INCHES FROM OTBD END, AND 2.75 INCHES FROM AFT EDGE.
Part: PANEL — PUNCTURED (APU BAY) · airframe 55,540 hrs · 19,631 cycles
APU COMPARTMENT, RIGHT ELEVATOR INDEX PLATE HARDWARE PUNCTURING THROUGH INTERIOR COMPOSITE PANEL.
Part: SKIN — DEBONDED (LT WING SLAT) · airframe 55,540 hrs · 19,631 cycles
NR 5 SLAT UPPER SURFACE HAD A DISBONDED DENT THAT WAS OUT OF LIMITS, 47.5 INCHES FROM THE INBD END, AND 5 INCHES FROM THE T/E.
Part: SKIN PANEL — DENTED (VERTICAL STAB) · airframe 55,540 hrs · 19,631 cycles
DENT FOUND ON VERTICAL STABILIZER RIGHT SURFACE 12"AFT OF AUX SPAR FSS 231.0.
Earlier reports · 1999–2017 · 79 reports
2017
Part: WARNING LIGHT — INOPERATIVE (L1 DOOR) · airframe 55,410 hrs · 19,568 cycles
AIRCRAFT WAS NOT GROUNDED. SLIDE LIGHT AT 1L, INOPERATIVE. REPLACED L1 DOOR LIGHT PER FIM 25-66-00. ACCOMPLISHED SATISFACTORY OPERATIONAL CHECK.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 55,377 hrs · 19,557 cycles
AIRCRAFT WAS NOT GROUNDED. EMERGENCY LIGHT AT SEAT 15D INOPERATIVE. REPLACED 15D SEAT MOUNTED LIGHT PER AMM 33-51-11. ACCOMPLISHED SATISFACTORY OPERATIONAL CHECK.
Part: WEB — CORRODED (CARGO DOOR) · corrosion level 2 · airframe 55,100 hrs · 19,427 cycles
CORROSION ON INSIDE OF FORWARD CARGO DOOR AT LOWER WEB ON FORWARD AND AFT ENDS. REMOVED AND REPLACED WEB.
2016
Part: GIRT BAR — DIRTY (L4 DOOR) · airframe 54,078 hrs · 18,995 cycles
AIRCRAFT NOT GROUNDED. L4 DOOR EVACUATION SLIDE GIRT BAR ARM LEVER IS DIFFICULT TO MOVE. REMOVED DEBRIS AND LUBRICATED GIRT BAR DOOR SILL IAW AMM 52-10-00. OPERATIONAL CHECK GOOD.
Part: COVER — LOOSE (L3 DOOR SLIDE) · airframe 53,774 hrs · 18,869 cycles
L3 DOOR SLIDE COVER IS LOOSE. SECURED THE COVER CENTER LATCH STRAP IAW 25-66-01. OPERATIONAL CHECK GOOD.
2015
Part: FILTER — DIRTY (ZONE 100) · airframe 51,642 hrs · 17,988 cycles
AFTER TAKEOFF & FOR 10 - 15 MINUTES, ODOR WAS NOTED BY FLIGHT ATTENDANT & PILOTS. SMELLED LIKE MOLD OR MUSTY. DISSIPATED AFTER HIGHER HEAT LEVELS WERE SELECTED IN ALL 3 ZONES, 78 - 79 DEGREES INDICATED IN COMPARTMENT ZONES. REPLACED LT RECYCLE FAN AIR FILTER & FWD GALLEY FILTER. PERFORMED PACK OPERATIONS, CHECKED NORMAL. OK FOR SERVICE IAW MM 21-25-02.
Part: PLATE — CORRODED (RT HORIZ STAB) · corrosion level 2 · airframe 51,372 hrs · 17,884 cycles
RIGHT LOWER SPLICE PLATE OF HORIZONTAL STABILIZER IS CORRODED BEYOND LIMITS. REPAIRED SPLICE PLATE IAW EA 253610.
Part: DECK PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 51,372 hrs · 17,884 cycles
MAIN FLOOR DECK PLATE HAS MULTIPLE AREAS OF CORROSION FROM STATION 1681 TO 1720. R & R ENTIRE AFT DECK SHEAR PLATE IAW SRM 51-40-02, AARD 51-00-05-1 & DWG 148N2301.
Part: BULKHEAD — CRACKED (RT PYLON) · airframe 51,372 hrs · 17,884 cycles
RIGHT PYLON AFT BULKHEAD HOLE NR 4 ON AFT FACE HAS A CRACK INDICATION IN THE ALUMINUM LAYER AT APPROX THE 2:00 O CLOCK POSITION. ENLARGED FASTENER HOLE IN THE ALUMINUM BULKHEAD ONLY TO 0.650 & INSTALLED ALUMINUM FREEZE PLUG & REAMED TO 0.4995. INSTALLED NEW FASTENER WITH RETENTION WASHER IAW EA 253355.
Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 51,372 hrs · 17,884 cycles
CORROSION ON TOP SURFACE OF CUSP AT STATION 1719 & LBL 56. R & R CUSP SECTION IAW DWG 146N8722 & 146N3700.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 50,452 hrs · 17,529 cycles
FORWARD EMER LIGHT ON SEAT 5E INOPERATIVE. REPLACED FWD EMER LIGHT ASSEMBLY AT SEAT 5E IAW AMM 33-51-01. SYS CHECKED NORMAL.
2014
Part: MODULE — DEFECTIVE (ZONE 300) · airframe 49,605 hrs · 17,219 cycles
TAKEOFF ABORTED. MASTER WARNING LIGHT ILLUMINATED & WARNING HORN SOUNDED DURING TAKEOFF AT 110 KNOTS. RED STABILIZER MSG APPEARED MOMENTARILY. ACCOMPLISHED FIM 27-09-00-815-811, FIM 27-09-00-815-803 & CARD 05-96-28 WITH NO FAULTS FOUND. FLIGHT DATA RECORDER DOWNLOAD INDICATED CTR STABILIZER TRIM LIMIT & POSITION TRANSMITTER MODULE FAULTS. R & R CTR LIMIT SWITCH & POSITION TRANSMITTER MODULE IAW AMM 27-48-01. PERFORMED OPERATIONAL CHECK IAW AMM 27-48-00. SYS CHECKED NORMAL.
Part: LIGHT — INOPERATIVE (L4 DOOR) · airframe 48,646 hrs · 16,853 cycles
LEFT NR 4 DOOR EMER SLIDE LIGHT FAILED TO TEST. REPLACED LAMP FOR LT NR 4 DOOR EMER SLIDE LIGHT. OPERATIONS CHECKED NORMAL.
Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 48,646 hrs · 16,853 cycles
LEFT NR 4 DOOR EXTERIOR EMER LIGHT INOPERATIVE. REPLACED LAMP FOR LT NR 4 DOOR EXTERIOR EMER LIGHT. OPERATIONS CHECKED NORMAL.
Part: PLACARD — WORN (CABIN) · airframe 47,772 hrs · 16,558 cycles
ARROW AT RT NR 1 DOOR WORN. REPLACED DECAL AT RT NR 1 DOOR. OPERATIONS CHECKED NORMAL.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 47,772 hrs · 16,558 cycles
OVERHEAD EMERGENCY LIGHT AT SEAT 16C INOPERATIVE. REPLACED LAMP FOR OVERHEAD EMERGENCY LIGHT AT SEAT 16C. OPERATIONS CHECKED NORMAL.
Part: PLACARD — WORN (CABIN) · airframe 47,772 hrs · 16,558 cycles
ARROW AT ROW 18DEF FOR EMERGENCY EXIT WORN. REPLACED DECAL FOR EMERGENCY EXIT AT 18DEF. OPERATIONS CHECKED NORMAL.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 47,772 hrs · 16,558 cycles
OVERHEAD EMERGENCY LIGHT AT SEAT 2E INOPERATIVE. REPLACED LAMP FOR OVERHEAD EMERGENCY LIGHT AT SEAT 2E. OPERATIONS CHECKED NORMAL.
Part: LIGHT — INOPERATIVE (L4 DOOR) · airframe 47,772 hrs · 16,558 cycles
LEFT NR 4 DOOR SLIDE LIGHT INOPERATIVE. REPLACED LAMP FOR SLIDE LIGHT AT LT NR 4 DOOR. OPERATIONS CHECKED NORMAL.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 47,772 hrs · 16,558 cycles
OVERHEAD HATCH LIGHT AT ROW 17DEF INOPERATIVE. REPLACED LAMP FOR OVERHEAD HATCH LIGHT AT ROW 17DEF. OPERATIONS CHECKED NORMAL.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 47,772 hrs · 16,558 cycles
OVERHEAD EMERGENCY LIGHT AT SEAT 5E INOPERATIVE. REPLACED LAMP FOR OVERHEAD EMERGENCY LIGHT AT SEAT 5E. OPERATIONS CHECKED NORMAL.
2013
Part: BOTTLE — NO TEST (EVAC SLIDE) · airframe 46,800 hrs · 16,221 cycles
EMERGENCY ESCAPE SLIDE TEST DOES NOT TEST IN POSITION 2. REPLACED OFF WING ESCAPE SLIDE SYSTEM PRESSURE BOTTLE. OPERATIONS CHECKED NORMAL.
Part: FAN — MALFUNCTIONED (CABIN) · airframe 46,544 hrs · 16,132 cycles
ADZ INFLIGHT SJO-MIA CREW REPORTED SMOKE ODOR IN THE CABIN & COCKPIT. EMERGENCY DECLARED FLIGHT DIVERTED ADZ LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. PLACARDED RT CABIN RECIRCULATION FAN IAW MEL 21-1A. REPLACED FAN AT LAX ON 09/20/2013. SYSTEM GROUND CHECKED NORMAL OPERATION CLOSED.
Part: ACCESS DOOR — GOUGED (FUSELAGE) · airframe 44,843 hrs · 15,521 cycles
ACCESS DOOR 113AL HAS GOUGES IN BOTH LEFT DOOR STOP CASTINGS. ACCOMPLISHED REPAIR PER EA B757-53-028722.
Part: PRESSURE DECK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 44,843 hrs · 15,521 cycles
MAIN CABIN FLOOR PRESSURE DECK CORRODED IN SEVERAL AREAS AT BODY STATION 1720, LEFT BUTTLINES 0 TO 54. REMOVED CORROSION PER SRM 53-60-51 AND REPAIRED DECK PLATE PER SRM 53-60-51-2R. REMOVED AND RE-INSTALLED L ANGLES PER SRM 51-40-02.
Part: STIFFENER — CRACKED (RT MLG WW) · airframe 44,843 hrs · 15,521 cycles
RIGHT MAIN WHEEL WELL, VERTICAL STIFFENER CRACKED AT INBOARD END BODY STATION 1180. REPLACED STIFFENER PER B757 SRM 51-40-02 AND BOEING DWG 144N2503.
Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 44,843 hrs · 15,521 cycles
MAIN CABIN RIGHT NUMBER 4 DOOR SILL AREA FLOOR SUPPORT STRUCTURE CORRODED AROUND FASTENER HOLES FROM BODY STATIONS 1660 TO 1680. REMOVED AND REPLACED SUPPORT STRUCTURE AT STATIONS 1660 TO 1680 PER SRM 51-40-02-0G.
Part: RECEPTACLE — GOUGED (FUSELAGE) · airframe 44,843 hrs · 15,521 cycles
ACCESS DOOR 113AL FORWARD LATCH PIN RECEPTICAL HAS GOUGE IN CASTING. REMOVED EDGE DAMAGE PER SRM 51-10-02. FLAP PEENED AREA, ALODINED, PRIMED AND PAINTED PER EA B757-52-028721.
Part: PRESSURE DECK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 44,843 hrs · 15,521 cycles
MAIN CABIN FLOOR PRESSURE DECK CORRODED IN SERVERAL AREAS THROUGHOUT BODY STATION 1720, RIGHT BUTTLINES 0 TO 54. REMOVED CORROSION PER SRM 53-60-01 AND REPAIRED DECK PLATE PER SRM 53-60-51-2. REMOVED AND REPLACED THREE CORRODED ANGLES PER SRM 51-40-02.
2012
Part: TRU — INOPERATIVE (ELECTRICAL SYS) · airframe 42,312 hrs · 14,579 cycles
BOS - CREW REPORTED FORWARD CARGO DOOR EICAS MESSAGE IN FLIGHT. EMERGENCY DECLARED FLIGHT RETURNED BOS LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. DEFERRED FORWARD CARGO DOOR ELECTRICAL DRIVE INOPERATIVE PER MEL. REPLACED GROUND SERVICE BUSS TRANSFORMER RECTIFIER UNIT AND LOCK SENSOR AT MIA ON 03/17/2012. SYSTEM GROUND CHECK NORMAL OPERATION.
2011
Part: WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 40,880 hrs · 14,024 cycles
CORROSION ON CENTER WEB STATION 1100 AROUND HYDRAULIC FITTING RIGHT MAIN LANDING GEAR WHEEL WELL. CUT OUT DAMAGED SECTION AND INSTALL A DOUBLER PER EA B757-53-019270.
Part: RELAY — FAULTY (HYDRAULIC SYS) · airframe 40,019 hrs · 13,717 cycles
MIA - CREW REPORTED RIGHT ENGINE HYDRAULIC LOW PRESSURE LIGHT ILLUMINATED. EMERGENCY DECLARED FLIGHT RETURNED MIA LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED TIMED RELAY K10560 THAT WAS FAULTY. SYSTEM GROUND CHECK NORMAL OPERATION.
2010
Part: DRAIN LINE — DISCONNECTED (GALLEY) · airframe 38,562 hrs · 13,168 cycles
MIA - CREW REPORTED DURING CLIMB RIGHT GENERATOR TRIPPED AND STRONG ELECTRICAL SMELL THROUGHOUT THE CABIN. EMERGENCY DECLARED FLIGHT RETURNED MIA LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. FOUND DRAIN HOSE FROM FIRST CLASS GALLEY DISCONNECTED CAUSING WATER DAMAGE TO 2 ELECTRICAL LOAD CONTROL UNITS. REPLACED UNITS AND CIRCUIT BREAKERS. SYSTEM GROUND CHECK NORMAL OPERATION (CLOSED)
Part: LIGHT — INOPERATIVE (CABIN) · airframe 38,322 hrs · 13,079 cycles
EMERGENCY LIGHTS AT SEAT 3E INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHTS AT SEAT 3E. OPS CHECK NORMAL.
Part: LENS — MISSING (CABIN) · airframe 38,324 hrs · 13,081 cycles
BULLNOSE EMERGENCY LIGHT AT SEAT 2EF MISSING LENS. REPLACED LENS FOR BULLNOSE EMERGENCY LIGHT AT SEAT 2EF. OPS CHECK NORMAL.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 38,324 hrs · 13,081 cycles
EMERGENCY LIGHTS AT SEAT 6E INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 6E. OPS CHECK NORMAL.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 38,324 hrs · 13,081 cycles
EMERGENCY LIGHTS AT SEAT 4E INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHTS AT SEAT 4E. OPS CHECK NORMAL.
Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 38,324 hrs · 13,081 cycles
EXTERIOR EMERGENCY LIGHT AT LEFT NUMBER 4 DOOR INOPERATIVE. REPLACED LAMP FOR EXTERIOR EMERGENCY LIGHT AT LEFT NUMBER 4 DOOR. OPS CHECK NORMAL.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 38,322 hrs · 13,079 cycles
EMERGENCY LIGHTS AT SEAT 2E INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHTS AT 2E. OPS CHECK NORMAL.
Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 36,837 hrs · 12,550 cycles
FORWARD SECTION OF COACH ESCAPE PATH LIGHTING INOPERATIVE. REPLACED BATTERY PACK AT FORWARD SECTION OF COACH FOR ESCAPE PATH LIGHTING. OPS CHECKED NORMAL.
Part: CHARGER — INOPERATIVE (CABIN) · airframe 36,837 hrs · 12,550 cycles
FORWARD SECTION OF COACH ESCAPE PATH LIGHTING INOPERATIVE. REPLACED CHARGER ASSEMBLY FOR BATTERY PACK AT FORWARD SECTION OF COACH.
Part: FLAP — CORRODED (WING) · corrosion level 2 · airframe 36,341 hrs · 12,363 cycles
CORROSION AT TOP SIDE OF INBOARD FLAP. LOCATED AT MID SEAM BETWEEN FASTENERS 2 INCHES FROM TRAILING EDGE AT INBOARD END. REPORTED CENTERBORE HONEYCOMB THAT WAS REMOVED TO SHOOT EXTERNAL DOUBLER POTTED CENTERBORE AND HOT BONDED DOUBLER PER SRM 51-70-10-2R PARAGRAPH 4D AND FIGURE 202.
Part: SKIN PANEL — CORRODED (TE FLAP) · corrosion level 2 · airframe 36,341 hrs · 12,363 cycles
CORROSION AT AFT EDGE FASTENER ROW OF INTERSPAR UPPER SKIN PANEL 52 INCHES FROM INBOARD END OF LEFT HAND MAIN INBOARD FLAP. REPAIRED CENTERBORE HONEYCOMB THAT WAS REMOVED TO SHOOT EXTERNAL DOUBLER POTTED CENTERBORE AND HOT BONDED DOUBLER PER SRM 51-70-10-2R PARAGRAPH 4D AND FIGURE 202.
Part: SLAT — DENTED (LT WING) · airframe 36,341 hrs · 12,363 cycles
DENT ON POSITION 9 SLAT, LEADING EDGE SLAT DENT 3.5 X 4 X .058 INCHES ON THE TRAILING EDGE 2 INCHES FROM THE TRAILING EDGE. DAMAGED CORE REMOVED AND NEW CORE INSTALLED AND HOT BONDED PER SRM 51-70-10-2R.
Part: GATE — CORRODED (L4 DOOR) · corrosion level 2 · airframe 36,341 hrs · 12,363 cycles
LEFT NUMBER 4 PASSENGER SERVICE DOOR GATE HAS CORROSION ON LOWER AFT CORNER. REMOVED CORRODED LOWER GATE AND INSTALLED NEW LOWER GATE PER ESO 90108.
Part: MOUNT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 36,341 hrs · 12,363 cycles
LAVATORY AFT INBOARD MOUNT HAS CORROSION. LAVATORY FLOOR FITTING WAS REMOVED AND REPLACED PER SRM 51-10-02-0G.
2009
Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 35,228 hrs · 11,976 cycles
FIRST CLASS EMERGENCY EGRESS LIGHTING FAILED FUNCTIONAL TEST. REPLACED BATTERY PACK FOR FIRST CLASS EMERGENCY LIGHT.
Part: LENS — MISSING (CABIN) · airframe 34,476 hrs
LGAM - SEAT 27D EMERGENCY EXIT LIGHT MISSING LENS. REPLACED LENS FOR SEAT 27D EMERGENCY EXIT LIGHT.
Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 34,584 hrs · 11,739 cycles
CABIN INTERCOSTAL CRACKED. REPAIRED IAW SRM 51-10-02-06.
2008
Part: LENS — MISSING (CABIN) · airframe 31,708 hrs
DFW EMERGENCY LIGHT AT SEAT 10D MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 10D. SYSTEM GROUND CHECKED NORMAL OPS. (CLOSED)
Part: LENS — MISSING (CABIN) · airframe 31,708 hrs
DFW EMERGENCY LIGHT AT SEAT 31C BULLNOSE MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 31C BULLNOSE. SYSTEM GROUND CHECKED NORMAL OPS. (CLOSED)
Part: LIGHT — INOPERATIVE (CABIN)
DFW - EMERGENCY LIGHT AT OVERHEAD EXIT AT SEAT 18A INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT OVERHEAD EXIT AT SEAT 18A. SYSTEM GROUND CHECKED NORMAL OPERATION. (A)
Part: LENS — MISSING (CABIN)
DFW - EMERGENCY LIGHT AT SEAT 33D MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 33D. SYSTEM GROUND CHECKED NORMAL OPERATION. (A)
Part: LIGHT — INOPERATIVE (EXTERIOR)
DFW - EXTERNAL EMERGENCY LIGHT AT LEFT HAND AFT DOOR INOPERATIVE. REPLACED LAMP FOR EXTERNAL EMERGENCY LIGHT AT LT AFT DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (A)
Part: PLACARD — DAMAGED (CABIN)
DFW - EMERGENCY LIGHT EXIT ARROW DECAL AT FORWARD SEAT 18A DAMAGED. REPLACED EXIT ARROW DECAL FOR EMERGENCY LIGHT AT FORWARD SEAT 18A. SYSTEM GROUND CHECKED NORMAL OPERATION. (A)
Part: LIGHT — INOPERATIVE (CABIN)
DFW - EMERGENCY LIGHT AT SEAT 24D INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 24D. SYSTEM GROUND CHECKED NORMAL OPERATION. (A)
2007
Part: MODULE — INOPERATIVE (EMERGENCY LIGHTS)
MIA - EMERGENCY LIGHT ALONG FLOOR AT LAST 10 ROWS OF COACH FLICKERED DURING TAKEOFF AND REMAINED OFF DURING CLIMB. ALL INDICATIONS NORMAL. REPLACED MODULE FOR EMERGENCY LIGHTS AT LAST 10 ROS OF COACH. SYSTEM GROUND CHECKED NORMAL OPERATION.
2006
Part: LIGHT — INOPERATIVE (CABIN)
JFK - EMERGENCY LIGHTS AT SEAT 4E MISSING LENS AND BULBS. REPLACED EMERGENCY LIGHT ASSEMBLY AT SEAT 4E. SYSTEM GROUND CHECKED NORMAL OPERATION.
2005
Part: SLIDE — DEPLOYED (NR 4 DOOR)
CABIN SERVICES PERSONNEL OPENED LT NR 4 DOOR AND PARTIALLY DEPLOYED SLIDE FROM INSIDE AIRCRAFT. DOOR ASSIST BOTTLE DISCHARGED. SLIDE DEPLOYED BUT DID NOT INFLATE. REPLACED SLIDE AND DOOR ASSIST BOTTLE. SYSTEM GROUND CHECKED NORMAL OPERATION.
2004
Part: SLIDE — FAILED (L1 DOOR)
L1 SLIDE PARTIAL UNSUCCESSFUL DEPLOYMENT. DOOR DID NOT DISARM. SLIDE PACK FELL OUT ON JETBRIDGE. DOOR ASSIST BOTTLE DISCHARGED UPON ARRIVAL AT GATE WHEN DOOR WAS BEING OPENED BY GROUND CREW. REPLACED SLIDE AT DOOR ONE LT. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED)
2003
Part: CONTROL PANEL — DEFECTIVE (EMERGENCY LIGHT)
DURING OVERNIGHT MAINTENANCE, 'UNARMED LIGHT' ON EMERGENCY LIGHT PANEL DOES NOT ILLUMINATE IN THE 'OFF' POSITION. REPLACED EMERGENCY LIGHT PANEL ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
Part: SPRING — DAMAGED (GIRT BAR)
TUL - DURING ACCOMPLISHMENT OF ENGINEERING REQUEST TO CHECK GIRT BAR SPRINGS AT EACH PASSENGER DOOR POSITION, ONE GIRT BAR SPRINGS NEEDED REPLACING. REPLACED ONE GIRT BAR SPRING. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
Part: LIGHT — LOOSE (CABIN)
MIA - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT STRIP FROM 4E-6E INOPERATIVE. RECONNECTED EMERGENCY EXIT LIGHT STRIP. SYSTEM GROUND CHECKED NROMAL OPERATION. (M)
Part: LIGHT — INOPERATIVE (CABIN)
DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTING AT ROWS 4-6 INOPERATIVE. PLUGGED IN EMERGENCY EXIT FLOOR PATH LIGHT STRIP AT ROW 4-6. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
Part: CONNECTOR — INOPERATIVE (EMERGENCY LIGHT)
JFK - DURING OVERNIGHT MAINTENANCE, FIRST CLASS EMERGENCY EXIT FLOOR LIGHT SECTION INOPERATIVE. REPLACED FIRST CLASS EMERGENCY EXIT FLOOR LGIHT WIRE CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
Part: LIGHT — INOPERATIVE (EXIT SIGN)
DURING OVERNIGHT MAINTENANCE, LT AFT EMERGENCY EXIT HATCH LIGHT INOPERATIVE. REPLACED EMERGENCY EXIT HATCH LIGHT ASSEMBLY. SYSTEM GRUOND CHECKED NORMAL OPERATION. (M)
Part: LIGHT — INOPERATIVE (CABIN)
ORD - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHTING AT ROWS 4-6 INOPERATIVE. REPLACED EMERGENCY EXIT LIGHTING STRIP. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
Part: LIGHT — INOPERATIVE (CABIN)
DFW - DURING OVERNIGHT MAINTENANCE, FIRST CLASS EMERGENCY EXIT FLOOR PATH LIGHTING FROM 4E-6E INOPERATIVE. RECONNECTED EMERGENCY EXIT FLOOR PATH LIGHT STRIP. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
Part: STRIP — DISCONNECTED (CABIN)
JFK - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT PATH FROM 3EF-7EF INOPERATIVE. RECONNECTED EMERGENCY EXIT LIGHT STRIP. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
2002
Part: CONNECTOR — LOOSE (CABIN)
JFK - DURING OVERNIGHT MAINTENANCE, FLOOR MOUNTED EMERGENCY EXIT LIGHTS IN FIRST CLASS INOPERATIVE. SECURED LOOSE CONNECTOR AT SEAT 1E. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
Part: CONNECTOR — LOOSE (CABIN)
MIA - FOUND FLOOR EMERGENCY LIGHTS IN FIRST CLASS ARE INOPERATIVE. REPAIRED LOOSE CONNECTION NEAR SEAT 1E. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
Part: CONNECTOR — LOOSE (CABIN)
MIA - FOUND EMERGENCY ESCAPE PATH LIGHTING STRIP ALONG RIGHT SIDE FROM SEAT 4E TO 6E INOPERATIVE. SECURED LOOSE CONNECTOR ON EMERGENCY PATH LIGHTING STRIP UNDER SEAT 5E. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
Part: CONNECTOR — FAULTY (CABIN)
JFK - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
2001
Part: HARNESS — DISCONNECTED (CABIN)
SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT PATH LIGHTING AT ROWS 1 AND 2 INOPERATIVE. RECONNECTED WIRING HARNESS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
Part: LIGHT — MALFUNCTIONED (CABIN)
SJU - FLT 1888 - EN ROUTE SJU-BDL, ON TAKEOFF, ROLL EMERGENCY EXIT LIGHT ILLUMINATED IN CABIN. LIGHTS TURNED OFF AFTER TAKEOFF. LANDED BDL WITHOUT FURTHER INCIDENT. INSPECTED EMERGENCY EXIT LIGHT SYSTEM. NO DEFECTS NOTED. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
2000
Part: CONNECTOR — DAMAGED (CABIN)
JFK - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHT AT SEAT ROW 17 THROUGH 24 INOPERATIVE. REPAIRED EMERGENCY EXIT FLOOR PATH LIGHT CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
Part: WIRE — BROKEN (CABIN)
DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT ESCAPE PATH LIGHT AT R2 DOOR INOPERATIVE. REPAIRED WIRE AT R2 DOOR. SYSTEM GROUND CHECK NORMAL OPERATION. (M)
Part: WIRE — INOPERATIVE (CABIN)
ORD - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHTS IN FIRST CLASS INOPERATIVE. REPAIRED EMERGENCY EXIT LIGHT WIRING. SYSTEM GROUND CHECK NORMAL OPERATION. (M)
1999
Part: CONNECTOR — DEFECTIVE (CABIN)
SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTS BETWEEN SEATS 3E AND 6E INOPERATIVE. REPLACED CONNECTORS TO EMERGENCY EXIT FLOOR PATH LIGHT STRIPS BETWEEN SEATS 3E AND 6E. SYSTEM GROUND CHECK, NORMAL OPERATION. (X)